Consider a Hohmann Transfer Orbit to Venus.
Part a: Assuming circular orbits, what are the orbital
velocities for Earth and Venus?
Part b: What will the semi-major axis and period of the transfer
orbit be? How long will it take to get to Venus if you follow this
orbit?
Part c: What are the perihelion and aphelion velocities of the transfer orbit? So, by how much and in what direction do you need to adjust the velocity of the rocket at launch and at arrival?
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